# Yakovlev Yak 52TW — Yak52TW_W&B_steve_dalton

> **NOT FOR FLIGHT** — source fidelity: unreviewed | operational review: none | completeness: full

> **content_gap**: Section "Weight and Balance" item count differs between passes (43 vs 45); verify nothing was dropped.

## Weight and Balance

**Enter amounts in yellow cells**
**N52SD**
**S/N: 0112226**
**Date: 18 MAY 2002**
- [ ] Empty weight of Aircraft — **2264.3 lbs.**
- [ ] Empty weight of Aircraft arm — **46.170532614936185 in**
- [ ] Empty weight of Aircraft moment — **104543.937 in-lbs.**
- [ ] Oil (1.9 lb/qt) — **0 Quarts**
- [ ] Oil weight — **0 lbs.**
- [ ] Oil arm — **4.59 in**
- [ ] Oil moment — **0 in-lbs.**
- [ ] Main Fuel — **0 Gallons**
- [ ] Main Fuel weight — **0 lbs.**
- [ ] Main Fuel arm — **45.15 in.**
- [ ] Main Fuel moment — **0 in-lbs**
- [ ] Aux. Fuel — **0 Gallons**
- [ ] Aux. Fuel weight — **0 lbs.**
- [ ] Aux. Fuel arm — **71.76 in.**
- [ ] Aux. Fuel moment — **0 in-lbs**
- [ ] Smoke Oil — **0 Gallons**
- [ ] Smoke Oil weight — **0 lbs.**
- [ ] Smoke Oil arm — **65 in.**
- [ ] Smoke Oil moment — **0 in-lbs**
- [ ] Front Pilot — **0 lbs.**
- [ ] Front Pilot arm — **48.87 in**
- [ ] Front Pilot moment — **0 in-lbs**
- [ ] Rear Pilot — **0 lbs.**
- [ ] Rear Pilot arm — **99.48 in.**
- [ ] Rear Pilot moment — **0 in-lbs**
- [ ] Baggage — **0 lbs.**
- [ ] Baggage arm — **117.79 in.**
- [ ] Baggage moment — **0 in-lbs**
- [ ] Total weight — **2264.3 lbs.**
- [ ] Total arm — **46.170532614936185 in.**
- [ ] Total moment — **104543.937 in-lbs**
- [ ] Gear up? (YES or NO): — **NO**
- [ ] % M.A.C. — **0.22532956150009692**
- [ ] Within Normal Limits?: — **YES**
- [ ] Within Acro Limits?: — **YES**
> **NOTE:** Maximum Gross weight is 3,012 Lbs. (1,366 Kg.)
> **NOTE:** Aerobatic C.G. Limits (17.5% to 28% M.A.C.)
> **NOTE:** Normal C.G. Limits (17.5% to 31% M.A.C.)
> **NOTE:** Gear extension moves the C.G. aft .5% M.A.C.

## Weighing Information

**Enter weights in yellow cells**
- [ ] Left Main weight — **1086 lbs.**
- [ ] Left Main arm — **33.56 in.**
- [ ] Left Main moment — **36446.16 in-lbs**
- [ ] Right Main weight — **1082 lbs.**
- [ ] Right Main arm — **33.56 in.**
- [ ] Right Main moment — **36311.920000000006 in-lbs**
- [ ] Tail weight — **121 lbs.**
- [ ] Tail arm — **263.63 in.**
- [ ] Tail moment — **31899.23 in-lbs**
- [ ] Oil (1.9 lb/qt) — **13 qt.**
- [ ] Oil arm — **4.59 in**
- [ ] Oil moment — **113.373 in-lb**
- [ ] Main Fuel — **0 gal.**
- [ ] Main Fuel arm — **45.15 in.**
- [ ] Main Fuel moment — **0 in-lb**
- [ ] Aux. Fuel — **0 gal.**
- [ ] Aux. Fuel arm — **68.38 in.**
- [ ] Aux. Fuel moment — **0 in-lb**
- [ ] Empty Totals weight — **2264.3 lbs.**
- [ ] Empty Totals arm — **46.170532614936185 in.**
- [ ] Empty Totals moment — **104543.937 in-lbs**
> **NOTE:** Datum is front jacking point on firewall
> **NOTE:** Level aircraft using the front cockpit canopy rail

---

NOT FOR FLIGHT — source fidelity: unreviewed | operational review: none | completeness: full  
Source: Yakovlev/Yak 52TW/Yak52TW_W&B_steve_dalton.txt  
Rights: licensed  
Checklist hash: 5fed48ff1c8c57b303204711136bcc248ab3a20ad0612714da0687d99e8f5194  
Verify against the aircraft's own approved documentation before use.